EP2540851A1 - Extrusion of glassy aluminum-based alloys - Google Patents
Extrusion of glassy aluminum-based alloys Download PDFInfo
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- EP2540851A1 EP2540851A1 EP12162638A EP12162638A EP2540851A1 EP 2540851 A1 EP2540851 A1 EP 2540851A1 EP 12162638 A EP12162638 A EP 12162638A EP 12162638 A EP12162638 A EP 12162638A EP 2540851 A1 EP2540851 A1 EP 2540851A1
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- EP
- European Patent Office
- Prior art keywords
- glassy
- aluminum
- temperature
- alloy
- billet
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 54
- 239000000956 alloy Substances 0.000 title claims abstract description 54
- 238000001125 extrusion Methods 0.000 title claims abstract description 30
- 229910052782 aluminium Inorganic materials 0.000 title claims abstract description 26
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims abstract description 26
- 238000000034 method Methods 0.000 claims abstract description 33
- 238000002791 soaking Methods 0.000 claims abstract description 5
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 10
- 229910000838 Al alloy Inorganic materials 0.000 claims description 9
- 238000004031 devitrification Methods 0.000 claims description 6
- 229910052759 nickel Inorganic materials 0.000 claims description 5
- 229910052727 yttrium Inorganic materials 0.000 claims description 5
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 5
- 238000010438 heat treatment Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000012545 processing Methods 0.000 description 2
- 229910017709 Ni Co Inorganic materials 0.000 description 1
- 229910003267 Ni-Co Inorganic materials 0.000 description 1
- 229910003262 Ni‐Co Inorganic materials 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000007596 consolidation process Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 235000012438 extruded product Nutrition 0.000 description 1
- 238000007496 glass forming Methods 0.000 description 1
- 238000007731 hot pressing Methods 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 230000000930 thermomechanical effect Effects 0.000 description 1
- 229910052723 transition metal Inorganic materials 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/002—Extruding materials of special alloys so far as the composition of the alloy requires or permits special extruding methods of sequences
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C25/00—Profiling tools for metal extruding
- B21C25/02—Dies
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/11—Making amorphous alloys
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C21/00—Alloys based on aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
Definitions
- Aluminum alloys are important in many industries. Glassy Al-based alloys and their devitrified derivatives are currently being considered for structural applications in the aerospace industry. These alloys involve the addition of rare earth and transition metal elements. These alloys have high strength and, when processed appropriately, have high ductility.
- the alloys When aluminum or aluminum alloys are extruded, the alloys, depending on the alloy composition, are heated to between 700 °F (375 °C) and 800 °F (427 °C), and are extruded through shear-faced dies with a high extrusion ratio and at high ram speeds. This functions to impart as much "work” into the alloy as possible. There is no concern for adiabatic heating because the alloys are usually heat-treatable. The alloys can be solutionized, quenched and aged to a desirable temper after extrusion.
- Al-based alloys such as Al-Y-Ni-Co alloys are devitrified glass-forming aluminum alloys that derive their strength from a nanometer-sized grain structure and nanometer-sized intermetallic second phase or phases. Examples of such alloys are disclosed in co-owned U.S. Patents No, 6,974,510 and 7,413,621 . Both devitrified aluminum alloys with nanocrystalline microstructures and those that are glassy without being devitrified have not been successfully extruded using conventional extrusion practices.
- the present invention includes a process for extruding aluminum alloys that are initially at least partially glassy in powder or melt-spun ribbon, and those that are then devitrified during processing and are fully devitrified during the consolidation step, such as hot pressing and/or during extrusion.
- the extrusion process of this invention provides for retention of the nano-scale microstructure. Temperature and strain are minimized by the use of streamline dies under controlled conditions.
- aluminum based alloys containing from 3 to 18.5 atomic percent nickel and 3 to 14.0 atomic percent yttrium.
- the present invention provides a method of extruding a glassy aluminum-based alloy, comprising the steps of: selecting a aluminum-based alloy billet; soaking the billet for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F (148.9 °C to 315.6 °C); extruding the billet in a streamline die having an extrusion ratio sufficient to keep the adiabatic temperature below the starting temperature while maintaining the streamline die at a temperature of about 400 °F to about 600 °F (204.4 °C to 315.6 °C) at a ram speed less than that which would raise the streamline die temperature within this range; and removing the extruded billet from the die.
- FIG. 1 is a cross section of a streamlined die for extruding the aluminum devitrified alloys of this invention.
- FIG. 2 is a block flow diagram of the extrusion process of this invention.
- FIG. 1 illustrates a streamline die 10 for extrusion of aluminum alloys and other materials.
- Die 10 is effective in minimizing the effect of temperature and total strain on the extruded product. Die 10 promotes the elimination/minimization of redundant work, thereby lowering the total plastic strain. Consequently, adiabatic heating is also reduced.
- the extrusion ratio, the cross-section for output end 11 divided into the cross-section for input end 13, can range from 1.1 to 50, depending on the material being extruded. For the alloys used in this invention, optimum results are obtained with an extrusion ratio from about 10:1.
- the opening 15 of the output end 11 is slightly tapered to prevent smearing, so that the only contact by the billet on the die is in extrusion region 17.
- Working length 19 can range from 1 inch to sixty inches (2.5 to 150 cm), though the more effective ranges is 4 inches to 6 inches (10 to 15 cm).
- the alloys extruded by the present method are glassy aluminum based alloys, some of which are devitrified, having a nanocrystalline microstructure, and some of which remain glassy with substantially no devitrification.
- the appropriate glassy aluminum based alloy billet is selected in Step 111.
- the billets are heated in a soak furnace, Step 113, for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F (148.9 °C to 315.6 °C).
- the starting temperature is about 450 °F to about 550 °F (232.2 °C to 287.9 °C) and the soak time is from about 10 minutes to about 72 hours.
- the starting temperature is about 400 °F to about 575 °F (204.4 °C to 301.7 °C) and the soak time is from about 10 minutes to about 5 hours.
- Step 115 is the actual extrusion step, where the billet is extruded in a streamline die 10 having an extrusion ratio sufficient to keep the adiabatic temperature below the starting temperature while maintaining streamline die 10 at a temperature of about 400 °F to about 600 °F (204.4 °C to 315.6 °C) at a ram speed less than that which would raise the streamline die temperature within this range.
- the streamline die is maintained at a temperature ranging from about 400 °F to about 575 °F (204.4 °C to 301.7 °C) at a ram speed of from about 0.1 to 100 inches per minute (0.25 to 250 cm per minute).
- the streamline die is maintained at a temperature ranging from about 475 °F to about 525 °F (246.1 °C to 273.9 °C) at a ram speed of from about 0.1 to 5 inches per minute (0.25 to 13 cm per minute).
- Step 117 is a conventional step of removing the extrusion from die 10 via torching, shearing, etc.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Extrusion Of Metal (AREA)
Abstract
A method of extruding a glassy aluminum-based alloy billet, by soaking (113) the billet for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F and extruding (115) the billet in a streamline die having an extrusion ratio to keep the adiabatic temperature below the starting temperature while maintaining the streamline die at a temperature of about 400 °F to about 600 °F at a ram speed less than that which would raise the streamline die temperature within this range.
Description
- Aluminum alloys are important in many industries. Glassy Al-based alloys and their devitrified derivatives are currently being considered for structural applications in the aerospace industry. These alloys involve the addition of rare earth and transition metal elements. These alloys have high strength and, when processed appropriately, have high ductility.
- One of the key requirements for high ductility is control of the second phase size during thermomechanical processing; in this case, extrusion into various extruded shapes.
- When aluminum or aluminum alloys are extruded, the alloys, depending on the alloy composition, are heated to between 700 °F (375 °C) and 800 °F (427 °C), and are extruded through shear-faced dies with a high extrusion ratio and at high ram speeds. This functions to impart as much "work" into the alloy as possible. There is no concern for adiabatic heating because the alloys are usually heat-treatable. The alloys can be solutionized, quenched and aged to a desirable temper after extrusion.
- Because glassy Al-based alloys have different structures, the temperatures noted above along with adiabatic heating from the shear-faced dies promote almost instantaneous devitrification so that the benefits of the glassy state are lost. Also, derivatives of the glassy state produce nanocrystalline microstructures that have mechanical properties that cannot be obtained when starting out with powder in the crystalline state. Al-based alloys such as Al-Y-Ni-Co alloys are devitrified glass-forming aluminum alloys that derive their strength from a nanometer-sized grain structure and nanometer-sized intermetallic second phase or phases. Examples of such alloys are disclosed in co-owned
U.S. Patents No, 6,974,510 and7,413,621 . Both devitrified aluminum alloys with nanocrystalline microstructures and those that are glassy without being devitrified have not been successfully extruded using conventional extrusion practices. - A new approach to extrusion of glassy Al-based powder is needed.
- The present invention includes a process for extruding aluminum alloys that are initially at least partially glassy in powder or melt-spun ribbon, and those that are then devitrified during processing and are fully devitrified during the consolidation step, such as hot pressing and/or during extrusion. The extrusion process of this invention provides for retention of the nano-scale microstructure. Temperature and strain are minimized by the use of streamline dies under controlled conditions.
- Of particular use are aluminum based alloys containing from 3 to 18.5 atomic percent nickel and 3 to 14.0 atomic percent yttrium.
- The present invention provides a method of extruding a glassy aluminum-based alloy, comprising the steps of: selecting a aluminum-based alloy billet; soaking the billet for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F (148.9 °C to 315.6 °C); extruding the billet in a streamline die having an extrusion ratio sufficient to keep the adiabatic temperature below the starting temperature while maintaining the streamline die at a temperature of about 400 °F to about 600 °F (204.4 °C to 315.6 °C) at a ram speed less than that which would raise the streamline die temperature within this range; and removing the extruded billet from the die.
- Certain preferred embodiments will now be described in greater detail by way of example only and with reference to the accompanying drawings.
-
FIG. 1 is a cross section of a streamlined die for extruding the aluminum devitrified alloys of this invention. -
FIG. 2 is a block flow diagram of the extrusion process of this invention. -
FIG. 1 illustrates a streamline die 10 for extrusion of aluminum alloys and other materials. Die 10 is effective in minimizing the effect of temperature and total strain on the extruded product. Die 10 promotes the elimination/minimization of redundant work, thereby lowering the total plastic strain. Consequently, adiabatic heating is also reduced. The extrusion ratio, the cross-section foroutput end 11 divided into the cross-section forinput end 13, can range from 1.1 to 50, depending on the material being extruded. For the alloys used in this invention, optimum results are obtained with an extrusion ratio from about 10:1. The opening 15 of theoutput end 11 is slightly tapered to prevent smearing, so that the only contact by the billet on the die is inextrusion region 17. Workinglength 19 can range from 1 inch to sixty inches (2.5 to 150 cm), though the more effective ranges is 4 inches to 6 inches (10 to 15 cm). - The alloys extruded by the present method are glassy aluminum based alloys, some of which are devitrified, having a nanocrystalline microstructure, and some of which remain glassy with substantially no devitrification. As noted in
FIG. 2 , the appropriate glassy aluminum based alloy billet is selected inStep 111. - The billets are heated in a soak furnace,
Step 113, for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F (148.9 °C to 315.6 °C). When the alloy is a devitrified alloy, the starting temperature is about 450 °F to about 550 °F (232.2 °C to 287.9 °C) and the soak time is from about 10 minutes to about 72 hours. When the alloy is a glassy alloy, the starting temperature is about 400 °F to about 575 °F (204.4 °C to 301.7 °C) and the soak time is from about 10 minutes to about 5 hours. -
Step 115 is the actual extrusion step, where the billet is extruded in astreamline die 10 having an extrusion ratio sufficient to keep the adiabatic temperature below the starting temperature while maintainingstreamline die 10 at a temperature of about 400 °F to about 600 °F (204.4 °C to 315.6 °C) at a ram speed less than that which would raise the streamline die temperature within this range. When the alloy is a devitrified alloy, the streamline die is maintained at a temperature ranging from about 400 °F to about 575 °F (204.4 °C to 301.7 °C) at a ram speed of from about 0.1 to 100 inches per minute (0.25 to 250 cm per minute). When the alloy is a glassy alloy, the streamline die is maintained at a temperature ranging from about 475 °F to about 525 °F (246.1 °C to 273.9 °C) at a ram speed of from about 0.1 to 5 inches per minute (0.25 to 13 cm per minute). -
Step 117 is a conventional step of removing the extrusion from die 10 via torching, shearing, etc. - Use of the method of this invention has produced extruded parts from devitrified alloys that retain the nanocrystalline microstructure and, thus, the superior strength of those alloys. Similarly, the method of this invention has produced extruded parts from glassy aluminum alloys having substantially no devitrification, also without loss of the superior properties of these alloys.
- While the invention has been described with reference to an exemplary embodiment(s), it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention defined by the claims. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment(s) disclosed, but that the invention will include all embodiments falling within the scope of the appended claims.
- The following clauses set out features of the invention which may not presently be claimed in this application, but which may form the basis for future amendment or a divisional application.
- 1. A method of extruding a glassy aluminum-based alloy having substantially no devitrification, comprising the steps of:
- selecting a glassy aluminum-based alloy billet;
- soaking the billet for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F (148.9 °C to 315.6 °C);
- extruding the billet in a streamline die having an extrusion ratio sufficient to keep the adiabatic temperature below the starting temperature while maintaining the streamline die at a temperature of about 400 °F to about 600 °F (204.4 °C to 315.6 °C) at a ram speed less than that which would raise the streamline die temperature within this range; and
- removing the extruded billet from the die.
- 2. The method of clause 1, wherein the glassy aluminum based alloy is an aluminum based alloy containing from 3 to 18.5 atomic percent nickel and 3 to 14.0 atomic percent yttrium.
- 3. The method of clause 1, wherein the starting temperature is about 450 °F to about 550 °F (232.2 °C to 287.8 °C) and the soak time is from about 10 minutes to about 5 hours.
- 4. The method of clause 3, wherein the streamline die is maintained at a temperature ranging from about 475 °F to about 525 °F (246.1 °C to 273.9 °C) at a ram speed of from about 0.1 to 5 inches per minute.
- 5. The method of clause 4, wherein the streamline die has an extrusion ratio of from about 1 to about 10, and has a length ranging from about 4 inches to 6 inches (10.16 cm. to 15.24 cm.)
- 6. A method of extruding a devitrified glassy aluminum-based alloy, comprising the steps of:
- selecting a devitrified glassy aluminum-based alloy billet;
- soaking the billet for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F (148.9 °C to 315.6 °C);
- extruding the billet in a streamline die having an extrusion ratio sufficient to keep the adiabatic temperature below the starting temperature while maintaining the streamline die at a temperature of about 400 °F to about 600 °F (204.4 °C to 315.6 °C) at a ram speed less than that which would raise the streamline die temperature within this range; and
- removing the extruded billet from the die.
- 7. The method of clause 6, wherein the devitrified glassy aluminum based alloy is an aluminum based alloy containing from 3 to 18.5 atomic percent nickel and 3 to 14.0 atomic percent yttrium.
- 8. The method of clause 6, wherein the starting temperature is about 400 °F to about 575 °F (204.4 °C to 301.7 °C) and the soak time is from about 10 minutes to about 72 hours.
- 9. The method of clause 6, wherein the streamline die is maintained at a temperature ranging from about 400 °F to about 575 °F (204.4 °C to 301.7 °C) at a ram speed of from about 0.1 to 100 inches per minute.
- 10. The method of clause 6, wherein the streamline die has an extrusion ratio of from about 1 to about 10, and has a length ranging from about 4 inches to 6 inches (10.16 cm. to 15.24 cm.)
- 11. An alloy produced by the method of any preceding clause.
Claims (14)
- A method of extruding a glassy aluminum-based alloy, comprising the steps of:selecting (111) a aluminum-based alloy billet;soaking (113) the billet for sufficient time to heat the billet to an extrusion starting temperature of from about 300 °F to about 600 °F (148.9 °C to 315.6 °C);extruding (115) the billet in a streamline die having an extrusion ratio sufficient to keep the adiabatic temperature below the starting temperature while maintaining the streamline die at a temperature of about 400 °F to about 600 °F (204.4 °C to 315.6 °C) at a ram speed less than that which would raise the streamline die temperature within this range; andremoving (117) the extruded billet from the die.
- The method of claim 1, wherein the glassy aluminum based alloy is selected from the group consisting of a devitrified alloy having a nanocrystalline microstructure and a glassy aluminum alloy having substantially no devitrification.
- The method of claim 2, wherein the glassy aluminum is a devitrified alloy having a nanocrystalline microstructure.
- The method of claim 3, wherein the glassy aluminum based alloy is an aluminum based alloy containing from 3 to 18.5 atomic percent nickel and 3 to 14.0 atomic percent yttrium.
- The method of claim 3 or 4, wherein the starting temperature is about 450 °F to about 575 °F (232.2 °C to 301.7 °C) and the soak time is from about 10 minutes to about 72 hours.
- The method of claim 5, wherein the starting temperature is about 400 °F to about 550 °F (204.4 °C to 287.9 °C) and the soak time is from about 10 minutes to about 72 hours.
- The method of any one of claims 3 to 6, wherein the streamline die is maintained at a temperature ranging from about 400 °F to about 575 °F (204.4 °C to 301.7 °C) at a ram speed of from about 0.1 to 100 inches per minute (0.25 to 250 cm per minute).
- The method of claim 2, wherein the glassy aluminum is a glassy aluminum alloy having substantially no devitrification.
- The method of claim 8, wherein the glassy aluminum based alloy is an aluminum based alloy containing from 3 to 18.5 atomic percent nickel and 3 to 14.0 atomic percent yttrium.
- The method of claim 8 or 9, wherein the alloy is a glassy alloy, the starting temperature is about 400 °F to about 575 °F (204.4 °C to 301.7 °C) and the soak time is from about 10 minutes to about 5 hours.
- The method of claim 10, wherein the starting temperature is about 450 °F to about 550 °F (232.2 °C to 287.8 °C).
- The method of any one of claims 8 to 11, wherein the streamline die is maintained at a temperature ranging from about 475 °F to about 525 °F (246.1 °C to 273.9 °C) at a ram speed of from about 0.1 to 5 inches per minute (0.25 to 13 cm per minute).
- The method of any preceding claim, wherein the streamline die has an extrusion ratio of from about 1 to about 10, and has a length ranging from about 4 inches to 6 inches (10.16 cm. to 15.24 cm.)
- An extruded alloy produced by the method of any preceding claim.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/169,204 US8603267B2 (en) | 2011-06-27 | 2011-06-27 | Extrusion of glassy aluminum-based alloys |
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EP2540851A1 true EP2540851A1 (en) | 2013-01-02 |
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EP12162638A Withdrawn EP2540851A1 (en) | 2011-06-27 | 2012-03-30 | Extrusion of glassy aluminum-based alloys |
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US (1) | US8603267B2 (en) |
EP (1) | EP2540851A1 (en) |
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EP3019638B1 (en) | 2013-07-10 | 2020-03-18 | United Technologies Corporation | Aluminum alloy and manufacture method |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
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US6974510B2 (en) | 2003-02-28 | 2005-12-13 | United Technologies Corporation | Aluminum base alloys |
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US1290011A (en) | 1918-11-29 | 1918-12-31 | Alpha Products Company | Process of making castings of rare-earth metals and their alloys. |
CA1095387A (en) | 1976-02-17 | 1981-02-10 | Conrad M. Banas | Skin melting |
US4479293A (en) | 1981-11-27 | 1984-10-30 | United Technologies Corporation | Process for fabricating integrally bladed bimetallic rotors |
US4530229A (en) | 1983-05-26 | 1985-07-23 | United Technologies Corporation | Forging method and die package therefor |
JP2911673B2 (en) * | 1992-03-18 | 1999-06-23 | 健 増本 | High strength aluminum alloy |
US5435161A (en) * | 1993-10-22 | 1995-07-25 | Aluminum Company Of America | Extrusion method utilizing variable billet preheat temperature |
US7063741B2 (en) | 2002-03-27 | 2006-06-20 | General Electric Company | High pressure high temperature growth of crystalline group III metal nitrides |
JP2005528530A (en) * | 2002-04-24 | 2005-09-22 | ケステック イノベーションズ エルエルシー | Nanophase precipitation strengthened Al alloy processed via amorphous state |
US20080308197A1 (en) * | 2007-06-15 | 2008-12-18 | United Technologies Corporation | Secondary processing of structures derived from AL-RE-TM alloys |
US9194027B2 (en) | 2009-10-14 | 2015-11-24 | United Technologies Corporation | Method of forming high strength aluminum alloy parts containing L12 intermetallic dispersoids by ring rolling |
US20110091346A1 (en) | 2009-10-16 | 2011-04-21 | United Technologies Corporation | Forging deformation of L12 aluminum alloys |
-
2011
- 2011-06-27 US US13/169,204 patent/US8603267B2/en not_active Expired - Fee Related
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2012
- 2012-03-30 EP EP12162638A patent/EP2540851A1/en not_active Withdrawn
Patent Citations (2)
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US6974510B2 (en) | 2003-02-28 | 2005-12-13 | United Technologies Corporation | Aluminum base alloys |
US7413621B2 (en) | 2003-02-28 | 2008-08-19 | United Technologies Corporation | Aluminum base alloys |
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US20120325378A1 (en) | 2012-12-27 |
US8603267B2 (en) | 2013-12-10 |
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